[net.space] thrust in the atmosphere

STEINBERG@RUTGERS.ARPA (06/15/84)

From:  Louis Steinberg <STEINBERG@RUTGERS.ARPA>

From: JHEIMANN@BBNA.ARPA

	So if the velocity of exhaust gasses is slowed by air friction, then
	the amount of momentum transfered to this gas is reduced, and thrust
	is decreased.

But if you are considering the momentum transfered to the air by the exhaust
gasses (presumably after they leave the nozzle), then you must include
the momentum of the air in your conservation-of-momentum calculations.

I think the simplest way to think about it is to consider the momentum
of the exhaust gas as it leaves the nozzle.  This depends on the velocity
and mass of the gas, as was explained.  Assume in both cases that the
same amount of fuel is pumped into the reaction chamber and that essentially
all the fuel reacts.  Then you have the same mass of exhaust gass to get
rid of through the nozzle in either case.

So, what about the velocity?  As the original question points out, the pressure
in the reaction chamber will be higher in the atmosphere.  Thus the exhaust
gas will be more dense.  (I assume density in the nozzle depends at least
partly on density at either end of the nozzle.)  Since we are dumping the
same amount of mass out the nozzle per unit time, and the mass is more dense,
it doesn't have to move as fast.  (Imagine you want 5 cars per minute to go
past some point on the highway.  If the cars are closer together (more dense)
they have to be going slower to achieve this rate.)

Thus, mass is constant and velocity is lower so momentum is lower.
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